View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 40900U 15049B 22180.57347862 .00020802 00000-0 58507-3 0 9997
2 40900 97.3991 198.6176 0007142 228.5715 250.0767 15.36496197376470
Epoch (UTC): | 29 June 2022 13:45:48 |
Eccentricity: | 0.0007142 |
inclination: | 97.3991° |
perigee height: | 451 km |
apogee height: | 461 km |
right ascension of ascending node: | 198.6176° |
argument of perigee: | 228.5715° |
revolutions per day: | 15.36496197 |
mean anomaly at epoch: | 250.0767° |
orbit number at epoch: | 37647 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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